High temperature resistant propellant for oil and gas deep wells and preparation method thereof
A technology of high temperature resistance and propellant, applied in the direction of alkali metal composition, etc., can solve the problems of inability to use, and achieve the effect of good temperature resistance and excellent hydrolysis resistance
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[0036] The preparation method of the above-mentioned high-temperature-resistant solid propellant for oil and gas deep wells, the method is carried out according to the following steps:
[0037] Step 1, according to the formula ratio, by weight percentage, the high temperature resistant epoxy resin is 10.00% to 20.90%, the bisphenol A epoxy resin is 0 to 16.58%, and the epoxy resin active diluent is 4.75 to 13.03%. The agent boron trifluoride-amine complex is 0.50%, the defoamer is 0.03%, add it into the mixing pot, and pre-mix for 10 minutes;
[0038] Step 2: In terms of weight percentage, 30.00% to 58.00% of potassium perchlorate and 2.00% to 30.00% of 1,1'-dihydroxy-5,5'-bitetrazolium dihydroxylamine salt are added to the system of step 1, After mixing for 50 minutes, add diaminodiphenyl sulfone at a rate of 6.57% to 8.14%, and stop mixing after mixing for 15 minutes to obtain a syrup;
[0039] Step 3: pour the slurry obtained in step 2 into a mold, put it into a 130°C oven...
Embodiment 1
[0042] The high-temperature-resistant solid propellant for oil and gas deep wells in this embodiment is composed of the following raw materials in terms of weight percentage: 30.00% of potassium perchlorate, 30.00% of 1,1'-dihydroxy-5,5'-bitetrazole dihydroxylamine salt %, 4,4'-diaminodiphenylmethane tetraglycidylamine type epoxy resin is 14.40%, epoxy resin E-51 is 5.47%, o-cresyl glycidyl ether is 13.03%, accelerator boron trifluoride - 0.50% of the amine complex, 0.03% of the silicone resin, and 6.57% of diaminodiphenylsulfone.
[0043] Performance Testing:
[0044]Detonation heat is determined by GJB770B-2005 method 701.2 detonation heat and combustion heat constant temperature method.
[0045] The specific volume is measured according to GJB770B-2005 method 702.1 specific volume pressure sensor method.
[0046] The test method for high temperature resistance is: Ф20mm×20mm powder column (1) 3°C / min rise to 200°C, keep warm for 48h; (2) Temperature control point: the the...
Embodiment 2
[0053] The high-temperature-resistant solid propellant for oil and gas deep wells of this embodiment is composed of the following raw materials in terms of weight percentage: 35.00% of potassium perchlorate, 25.00% of HATO, 10.00% of TGDDM, 16.58% of epoxy resin E-51, and Cresyl glycidyl ether is 4.75%, accelerator boron trifluoride-amine complex is 0.50%, silicone resin is 0.03%, and diaminodiphenylsulfone is 8.14%.
[0054] The performance test method of the high-temperature-resistant solid propellant for oil and gas deep wells in this embodiment is the same as that in Embodiment 1, and the performance test results are shown in Table 2.
[0055] Table 2 The performance test results of Example 2
[0056]
[0057] It can be concluded from Table 2 that the propellant has moderate heat of detonation (ie, energy), moderate specific volume, and high temperature resistance, water resistance and salt water resistance all meet the performance requirements. Suitable for oil and ga...
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